REFUEL AND

PRESELECT REFUEL C 1 0 (M) May be inoperative provided:a) Fuel transfer system is verified operative, and b) Procedures are established and used for gravity

refueling. −20−2 MASTER VALVE CLOSED

Light (Refuel/Defuel Panel) C 1 0 (M) May be inoperative provided theREFUEL/DEFUEL SHUT−OFF VALVE is verified closed following refueling.

−40−1 Height Measuring Unit

(Magnetic Dipsticks) C 2 0 May be inoperative provided the fuel quantity isdetermined by other approved means. −40−2 Fuel TANK °C Temperature

Indication (on ESID) C 1 0 May be inoperative._NOTE:

If using JET B / JP−4 fuel, the maximum operating altitude should not exceed 20,000 feet.

−40−3 FUELING ON Caution Light C 1 0 (O) May be inoperative provided prior to each flight: a) The REFUEL/OFF/DEFUEL switch is confirmed

OFF, and

b) The Refuel/Defuel access panel is verified closed.

−40−4 TANK 1 AUX PUMP and TANK 2 AUX PUMP Advisory Lights

C 2 1 (O) May be inoperative provided:

a) The associated ENG FUEL PRESS caution light and Aux Fuel Pump are verified operative, and b) Both flight compartment FUEL QTY Indications

are verified operative, and

c) Operations are conducted in compliance with AFM Supplement 95, OPERATION WITH AN INOPERATIVE AUX PUMP ADVISORY LIGHT.

Rev 7 Sep 09/2015 28−1

Systems & Nos de Sequence système Numbers de série

1. Item− Article

2. Number installed− Nombre d’articles installés

3. Number required for dispatch− Nombre requis pour le départ

4. Remarks or Exceptions− Remarques ou exceptions

−40−5 #1 TANK FUEL LOW and #2 TANK FUEL LOW Caution Lights

C 2 1 (O) May be inoperative provided:

a) The associated flight compartment FUEL QTY Indication is verified operative and is periodically monitored during flight, and

b) The associated engine FF (Fuel Flow) Indication is verified operative.

−40−6 Refuel/Defuel/Transfer VALVE (OPEN/CLOSED) Advisory Lights

C 2 1 (M) May be inoperative provided the fuel transfer system and flight compartment FUEL QTY Indications are verified operative.

−40−7 External Refuel/Defuel

Panel FUEL QTY Indicators C 2 0 (M) May be inoperative provided the fuel quantity isdetermined by other approved means prior to each flight.

−40−8 REFUEL SHUTOFF TANK 1 and REFUEL SHUTOFF TANK 2 Advisory Lights

C 2 0 (M) May be inoperative provided the flight compartment FUEL QTY Indications are verified operative.

−40−9

***

APU FUEL VALVEAdvisory Light

1) (OPEN) C 1 0 (M) May be inoperative provided:

a) The OPEN light is extinguished, and

b) The CLOSED light is illuminated when the APU is selected OFF.

2) (CLOSED) D 1 0 (M) May be inoperative provided: a) APU is not operated, and

b) The APU fuel shut off valve is verified closed. −40−10 Flight Compartment Fuel

QTY Indications (on ESID) C 2 1 (M) May be inoperative provided:a) The fuel quantity is determined by other approved means prior to each flight,

b) The Fuel Flow Indications are operative, are monitored during flight, and fuel consumption is recorded,

c) TANK FUEL LOW caution light is operative, and d) Aircraft is dispatched with wing tanks balanced. −40−11 Fuel Inlet Temperature

Indications (on Engine Display)

A 2 1 (O) May be inoperative for one flight provided the TANK AUX PUMP Advisory Lights are operative.

28−2 Rev 7 Sep 09/2015

Systems & Nos de Sequence système Numbers de série

1. Item− Article

2. Number installed− Nombre d’articles installés

3. Number required for dispatch− Nombre requis pour le départ

4. Remarks or Exceptions− Remarques ou exceptions

28 FUEL (CONT’D)

29 HYDRAULIC POWER

−10−1 Parking/Emergency Brake

Accumulator Hand Pump C 1 0 May be inoperative provided accumulator pressure isverified prior to engine start. −10−2 HYD FSOV OPEN Indicator

Light C 2 1 (M) One may be inoperative provided:a) The associated HYD FSOV is verified open, and b) The associated HYD FSOV CLOSED indicator

light is verified operative. −30−1 HYD PRESS 1 and HYD

PRESS 2 Indications C 2 1 (M) May be inoperative provided:a) The associated ENG HYD PUMP Caution Light is verified operative, and

b) The associated HYD QTY Indication is verified operative.

−30−2 HYD PRESS STBY

Indication C 1 0 (O) May be inoperative provided:a) Normal operation of the Standby Hydraulic Pump is verified before each flight, and b) HYD PRESS 1 and HYD PRESS 2 Indications

are verified operative. −30−3 System #1 and #2 Nacelle

Reservoir Quantity Indicators

C 2 0 (M)(O) May be inoperative provided:

a) HYD QTY 1 and HYD QTY 2 Indications are verified operative, and

b) ENG HYD PUMP Caution Lights are verified operative.

−30−4 #1 STBY HYD PUMP HOT

Caution Light A 1 0 May be inoperative provided:a) STBY HYD PRESS Indication is operative, and b) Repairs are made within one flight day.

−30−5 HYD QTY 3 Indication C 1 0 (M) May be inoperative provided:

a) The System #3 Aft Fuselage Hydraulic Quantity Indicator is verified operative, and

b) Adequate fluid quantity is verified before each flight.

−30−6 System #3 Aft Fuselage

Hydraulic Quantity Indicator C 1 0 May be inoperative provided HYD QTY 3 Indication isoperative. Rev 7 Sep 09/2015 29−1

Systems & Nos de Sequence système Numbers de série

1. Item− Article

2. Number installed− Nombre d’articles installés

3. Number required for dispatch− Nombre requis pour le départ

4. Remarks or Exceptions− Remarques ou exceptions

−30−7 HYD PRESS 3 Indication C 1 0 (M#) May be inoperative provided:

a) The #3 HYD PUMP Caution Light is verified operative, and

b) The HYD QTY 3 Indication is verified operative. −30−8 PTU CNTRL ON Advisory

Light

1) Pre Modsum 4−126354 or 4−126425

a) PTU CNTRL ON

Advisory Light C 1 0 (O) May be inoperative provided:a) The HYD PRESS 2 indication is verified operative,

b) The #2 ENG HYD PUMP caution light is verified operative, and

c) The hydraulic Power Transfer Unit is verified operative prior to each flight.

2) Post Modsum 4− 126354 or 4−126425 a) PTU CNTRL ON

Advisory Light (White) C 1 0 May be inoperative provided Pressure Green CrossHatch Advisory Light is operative. b) PTU CNTRL FAIL

Advisory Light (Amber) C 1 0 May be inoperative provided Pressure Green CrossHatch Advisory Light is operative. c) PTU CNTRL pressure

Green Cross Hatch Advisory Light (Green)

C 1 0 (O) May be inoperative provided:

a) The HYD PRESS 2 indication is verified operative,

b) The #2 ENG HYD PUMP caution light is verified operative, and

c) The hydraulic Power Transfer Unit is verified operative prior to each flight.

−30−9 #1 ENG HYD PUMP and #2 ENG HYD PUMP Caution Lights

C 2 1 (M) May be inoperative provided:

a) The associated flight compartment HYD PRESS Indication is verified operative,

b) The associated ISOLATION VALVE is verified operative, and

c) The associated hydraulic pressure is periodically monitored.

29−2 Rev 7 Sep 09/2015

Systems & Nos de Sequence système Numbers de série

1. Item− Article

2. Number installed− Nombre d’articles installés

3. Number required for dispatch− Nombre requis pour le départ

4. Remarks or Exceptions− Remarques ou exceptions

29 HYDRAULIC POWER (CONT’D)

−30−10 HYD QTY 1 and HYD QTY

2 Indications C 2 1 (M) May be inoperative provided:a) The quantity is verified adequate prior to each flight,

b) The associated ENG HYD PUMP Caution Light and HYD PRESS Indication are verified operative,

c) The associated HYD ISO VLV Caution Light is verified operative, and

d) The associated Nacelle Hydraulic Quantity Indicator is verified operative.

−30−11 STBY HYD PRESS ON

Advisory Light C 1 0 (O) May be inoperative provided the HYD PRESSSTBY indication is verified operative. −30−12 #1 HYD FLUID HOT and #2

HYD FLUID HOT Caution Lights

B 2 1 (M#)(O) May be inoperative provided:

a) The associated HYD PRESS Indication is verified operative and is periodically monitored during flight,

b) Adequate steps are taken each flight day to ensure that an overheat condition has not occurred, and

c) The associated HYD QTY Indication is verified operative.

−30−13 HYD #3 ISOL VLV OPEN

Advisory Light C 1 0 (O) May be inoperative provided:a) The HYD PRESS 3 indication is operative, and b) The ELEVATOR PRESS caution light is

operative.

Rev 6 Mar 26/2014 29−3

Systems & Nos de Sequence système Numbers de série

1. Item− Article

2. Number installed− Nombre d’articles installés

3. Number required for dispatch− Nombre requis pour le départ

4. Remarks or Exceptions− Remarques ou exceptions

29 HYDRAULIC POWER (CONT’D)

30 ICE AND RAIN PROTECTION

−10−1 TAIL De−Ice Boots

Advisory Lights C 4 0 May be inoperative provided the flight is not conductedin known or forecast icing conditions. −10−2 DEICE PRESS Caution

Light C 1 0 May be inoperative provided the flight is not conductedin known or forecast icing conditions. C 1 0 (M) May be inoperative provided:

a) All De−Ice Boot Advisory Lights are verified operative, and

b) The DEICE PRESS Indicators are verified operative.

−10−3 DEICE PRESS Indicators C 2 0 May be inoperative provided the flight is not conducted in known or forecast icing conditions.

C 2 0 (M) May be inoperative provided:

a) All De−Ice Boot Advisory Lights are verified operative, and

b) The DEICE PRESS Caution Light is verified operative.

−10−4 Low Pressure Warning

Switches (LPWS) C 2 1 (M#) May be inoperative provided:a) DEICE PRESS Caution Light is verified operative,

b) DEICE PRESS Indicator is verified operative, c) All De−ice Advisory Lights are verified operative,

and

d) Faulty LPWS is disconnected.

C 2 0 May be inoperative provided flight is not conducted in known or forecast icing conditions.

−10−5 WING De−Ice Boots

Advisory Lights C 8 2 (O) May be inoperative provided:a) The left wing root de−icer boot advisory light and right wing root de−icer boot advisory light are verified operative,

b) The associated boot operation is visually monitored when in use, and

c) The appropriate wing inspection light(s) operate normally for night operation.

Rev 6 Mar 26/2014 30−1

Systems & Nos de Sequence système Numbers de série

1. Item− Article

2. Number installed− Nombre d’articles installés

3. Number required for dispatch− Nombre requis pour le départ

4. Remarks or Exceptions− Remarques ou exceptions

−10−6 Timer Monitor Unit (TMU,

Timer Function) C 1 0 (M#) May be inoperative provided:a) Flight is not conducted in known or forecast icing conditions,

b) PITOT HEAT 1, PITOT HEAT 2 and PITOT HEAT STBY are verified operative,

c) L AOA VANE HEAT and R AOA VANE HEAT are verified operative, and

d) ENGINE INTAKE HEATER 1 and 2 are verified operative.

NOTE:

AUTO mode of De−icer boots cycle will be inoperative.

−10−7 Airframe De−Icing System C 1 0 May be inoperative provided the flight is not conducted in known or forecast icing conditions.

−20−1 Engine Intake Bypass Door OPN and CLOSED

Advisory Lights

C 2 0 (M) May be inoperative provided:

a) Bypass Door operation is verified prior to each flight, and

b) The related engine intake heater indicator is verified operative.

C 2 0 May be inoperative provided:

a) Associated bypass door(s) remains closed, and b) Flight is not conducted in known or forecast icing

conditions. −20−2 ENGINE INTAKE HTR

Advisory Lights C 2 0 (M)(O) May be inoperative provided:a) The associated Heater(s) is verified operative prior to dispatch, and

b) Associated ENG ADPT HEAT Caution Light(s) is verified operative.

C 2 1 May be inoperative provided the flight is not conducted in known or forecast icing conditions.

−20−3 ENG ADPT HEAT 1 and ENG ADPT HEAT 2 Caution Lights

C 2 1 (M)(O) May be inoperative provided:

a) The associated heater is verified operative prior to dispatch, and

b) The associated ENGINE INTAKE HTR advisory light is verified operative and is periodically monitored.

30−2 Rev 7 Sep 09/2015

Systems & Nos de Sequence système Numbers de série

1. Item− Article

2. Number installed− Nombre d’articles installés

3. Number required for dispatch− Nombre requis pour le départ

4. Remarks or Exceptions− Remarques ou exceptions

30 ICE AND RAIN PROTECTION (CONT’D)

−20−4 Engine Intake Adapter

Heater Assemblies C 2 1 May be inoperative provided the flight is not conductedin known or forecast icing conditions. −30−1 Pitot/Static Heaters B 3 2 May be inoperative for DAY VMC provided:

a) There is no visible moisture, and

b) The flight is not conducted into known or forecast icing conditions.

−30−2 PITOT HEAT 1, PITOT HEAT 2 and PITOT HEAT STBY Caution Lights

B 3 0 (M) May be inoperative provided:

a) The flight is not conducted into known or forecast icing conditions, and

b) All other elements of the pitot heat systems are verified operative prior to each flight.

−40−1 Windshield Wipers C 2 0 May be inoperative provided the flight is not conducted in precipitation within five nautical miles of the airport of take−off or intended landing.

−40−2 Windshield Heaters A 3 1 May be inoperative provided:

a) The flight is not conducted in known or forecast icing conditions, and

b) Repairs are made within three flight days. Co−Pilot Heated

Windshield (Right Hand Windshield)

A 1 0 (M#)(O) May be inoperative for one day provided: a) The Pilot’s Side Window heating is operative, b) The Pilot Windshield (Left Hand Windshield)

heating is verified operative prior to dispatch, and

c) The flight is conducted in accordance with AFM Supplement 114, “OPERATION WITH ONE WINDSHIELD HEATING SYSTEM

INOPERATIVE”.

−60−1 Propeller De−icing System C 1 0 May be inoperative provided flight is not conducted in known or forecast icing conditions.

−60−2 PROPS Heat Advisory

Lights B 2 0 (O) May be inoperative provided:a) AC LOAD indication is operating and periodically monitored, and

b) the PROP DEICE caution light is operative. C 2 0 May be inoperative provided flight is not conducted in

known or forecast icing conditions.

Rev 7 Sep 09/2015 30−3

Systems & Nos de Sequence système Numbers de série

1. Item− Article

2. Number installed− Nombre d’articles installés

3. Number required for dispatch− Nombre requis pour le départ

4. Remarks or Exceptions− Remarques ou exceptions

30 ICE AND RAIN PROTECTION (CONT’D)

−80−1 Ice Detector Spigot

Illumination Lights C 2 1 One may be inoperative at either the pilot’s or co−pilot’s position. C 2 0 May be inoperative for day operations.

A 2 0 (M) May be inoperative for night operations for one flight day provided:

a) Both Ice Detector Probes are operative, b) The flight is not conducted in known or forecast

icing conditions, and

c) A flashlight of adequate capacity is available and confirmed operable prior to each flight.

−80−2 Ice Detector Probes

(Electronic) A 2 1 (M)(O) May be inoperative for thirty days. B 2 0 (M)(O) Both may be inoperative provided:

a) Windshield wipers are stored in the normal horizontal position, and

b) Both Ice Detector Spigot illumination lights are confirmed operative prior to night operations. c) Flight will be conducted in accordance with AFM

Supplement Number 98, Operation with Both Ice Detector Probes (Electronic) inoperative (ICE DETECT FAIL caution Light Illuminated). d) The flight is not conducted at night into known or

forecast icing conditions.

30−4 Rev 7 Sep 09/2015

Systems & Nos de Sequence système Numbers de série

1. Item− Article

2. Number installed− Nombre d’articles installés

3. Number required for dispatch− Nombre requis pour le départ

4. Remarks or Exceptions− Remarques ou exceptions

30 ICE AND RAIN PROTECTION (CONT’D)

31 INDICATING AND RECORDING SYSTEMS

−20−1 Clocks

1) Pilot Clock A 1 0 May be inoperative provided:

a) Reliable and functioning timepiece is readily available to all Flight Compartment crew members, and

b) Repairs are made within three flight days. 2) Co−pilot Clock C 1 0 May be inoperative.

−30−1 Flight Data Recorder A 1 0 (M) May be inoperative provided:

a) The Cockpit Voice Recorder is operative, and b) Repairs are made within three flight days. 1) DFDR Recording

Parameters required by Regulation

A − − (M#) Up to three (3) digital recording parameters may be inoperative provided:

a) The Cockpit Voice Recorder is operative, and b) Repairs are made within twenty calendar days. 2) DFDR Recording

Parameters not required by Regulation

A − − (M#) May be inoperative provided repairs are made before completion of the next heavy maintenance check.

−30−2

***

Extended Quick AccessRecorder D − 0 (M) May be inoperative. −51−1 Caution and Warning Lights

System

1) Dual Master Caution switchlight (Glareshield, light function only) (CR833CH00034)

C 2 1 One may be inoperative.

2) Dual Master Warning Switchlight (Glareshield, light function only) (CR833CH00034)

C 2 1 One may be inoperative.

Rev 6 Mar 26/2014 31−1

Systems & Nos de Sequence système Numbers de série

1. Item− Article

2. Number installed− Nombre d’articles installés

3. Number required for dispatch− Nombre requis pour le départ

4. Remarks or Exceptions− Remarques ou exceptions

−60−1 ESID Control Panel 1) System Page Push

Button Switches C 4 0 (O) The ELEC SYS, ENG SYS, FUEL SYS, andDOORS SYS Switches may be inoperative provided the ALL Switch is operative.

31−2 Rev 7 Sep 09/2015

Systems & Nos de Sequence système Numbers de série

1. Item− Article

2. Number installed− Nombre d’articles installés

3. Number required for dispatch− Nombre requis pour le départ

4. Remarks or Exceptions− Remarques ou exceptions

31 INDICATING AND RECORDING SYSTEMS (CONT’D)

2) ALL Switch C 1 0 (O) The ALL Switch may be inoperative provided the ELEC SYS, FUEL SYS, ENG SYS and DOORS SYS Switches are operative.

3) Engine Display

Dimming Function C 1 0 Dimming may be inoperative provided the displayintensity is adequate. −60−2 MFD and PFD Engine

Display Messages 1) PFD 1 / 2 LINK FAIL

Engine Display message C 2 1 Message may be displayed. 2) MFD 1 / 2 LINK FAIL

Engine Display message C 2 1 Message may be displayed. −60−3 Electronic Flight Instrument

System Control Panels C 2 1 One panel may be inoperative provided:a) The pilot flying panel is fully operative, and b) Affected side must meet navigational

requirements for route being flown.

Bright/Dim Controls C 6 0 Dimming may be inoperative provided the display intensity is adequate.

−60−4 FADEC 1 / DU or FADEC 2 / DU Engine Display Message

A 2 1 Message may be annunciated for three flight days.

−60−5 EFIS/ESID Display Units A 5 4 (M)(O) RH MFD (MFD2) may be inoperative provided: a) RNP AR approach is not being conducted, b) The left hand Electronic Flight Instrument

System Control panel (EFCP) and the Engine and System Integrated Display Control Panel (ESCP) are fully functional,

c) The MFD1 rotary selector and ELEC SYS, ENG SYS, FUEL SYS, DOOR SYS and ALL push button switches are operative, and

d) Repairs are made within one flight day. NOTE:

The pilot occupying the left seat must conduct all departures and arrivals in Instrument

Meteorological Conditions.

Rev 7 Sep 09/2015 31−3

Systems & Nos de Sequence système Numbers de série

1. Item− Article

2. Number installed− Nombre d’articles installés

3. Number required for dispatch− Nombre requis pour le départ

4. Remarks or Exceptions− Remarques ou exceptions

31 INDICATING AND RECORDING SYSTEMS (CONT’D)

32 LANDING GEAR

−20−1

***

NOSE GEAR LOCK

Advisory Light D 1 0 May be inoperative provided Nose Gear Lock is verified disengaged prior to each departure. −30−1 Landing Gear Retraction

System A 1 0 (O) Landing gear retraction system may beinoperative for one flight provided operations are conducted in compliance with AFM Supplement 94, OPERATION WITH LANDING GEAR EXTENDED. −40−1 Parking Brake Pressure

Indications

In document Dash 8 Series 400, DOT, Master Minimum Equipment List, PSM A. (Page 83-97)